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Shape Memory Alloy Morphing Airfoil Sections

机译:形状记忆合金变形翼型部分

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Shape memory alloys (SMA) provide common solid state actuators with reliable and unique characteristics. Their special behavior is based on a reversible phase transformation and can provide high power density, induced strain and block force which render them indispensable for use in morphing structures that require large shape changes while space and weight restrictions are imposed. Yet, their implementation into morphing structures faces challenges related to their complex multi-disciplinary behavior, their interaction with the passive structural components, geometrical nonlinearity due to large shape changes, the lack of experimental data, and above all, the lack of modelling tools which can robustly simulate the complex thermomechanical behavior and make feasible their design. We briefly review the material characterization process, the developed modelling tools which can simulate the complex thermomechanical response of morphing structures with SMA actuators which can undergo large shape changes under severe geometric nonlinearity, and the testing of prototype morphing components. The design and validation of two morphing structural concepts for curvature control are presented. A morphing strip capable to deform towards a single target shape is initially presented. Subsequently, a morphing airfoil concept implementing an articulated mechanism capable to achieve multiple target shapes for aerodynamic load control is presented. The challenging task to continuously adapt the structural shape to time varying demands, dictates the use of antagonistic actuator configurations to maximize and control the range of morphing. The previously mentioned morphing airfoil configuration is used to alleviate the aerodynamic fatigue loads in wind turbine blades and aircraft wings.
机译:形状记忆合金(SMA)提供具有可靠和独特特性的常用固态执行器。它们的特殊行为基于可逆相变,可以提供高功率密度,诱导应变和阻力,这使得它们不可或缺于在需要大形状变化的变形结构中,同时施加空间和重量限制。然而,他们进入变形结构的实施面临与复杂的多学科行为相关的挑战,它们与被动结构部件的互动,几何非线性由于大的形状变化,实验数据缺乏,最重要的是缺乏建模工具可以强大地模拟复杂的热机械行为,并制作他们的设计。我们简要介绍了材料表征过程,所开发的建模工具,其可以模拟变形结构与SMA致动器的复杂热机械响应,该SMA致动器可以在严重的几何非线性下进行大规模变化,以及原型变形部件的测试。提出了两个变形结构概念的设计与验证。最初呈现能够朝向单个目标形状变形的变形条形。随后,提供了实现能够实现用于空气动力负载控制的多个目标形状的铰接机构的变形翼型概念。坚决性的任务来连续地适应结构形状与时间变化的需求,决定了使用拮抗致动器配置来最大化和控制变形范围。先前提到的变形翼型配置用于缓解风力涡轮机叶片和飞机翼中的空气动力学疲劳载荷。

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